View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 13403U 82079B 25189.53177130 .00003080 00000-0 13461-3 0 9998
2 13403 81.1487 120.6353 0024726 270.8985 88.9413 15.21519350340532
| Epoch (UTC): | 08 July 2025 12:45:45 |
| Eccentricity: | 0.0024726 |
| inclination: | 81.1487° |
| perigee height: | 484 km |
| apogee height: | 518 km |
| right ascension of ascending node: | 120.6353° |
| argument of perigee: | 270.8985° |
| revolutions per day: | 15.21519350 |
| mean anomaly at epoch: | 88.9413° |
| orbit number at epoch: | 34053 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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